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A.2
ENVIRONMENTAL QUALIFICATION FORM
NOMENCLATURE:
TYPE/MODEL/PART NO.:
TSO/JTSO COMPLIANCE:
MANUFACTURER'S SPECIFICATION AND/OR OTHER
APPLICABLE SPECIFICATION:
MANUFACTURER:
ADDRESS:
Conditions
Temperature and Altitude
Low Temperature
High Temperature
In-Flight Loss of Cooling
Altitude
Decompression
Overpressure
Temperature Variation
Humidity
Shock
Vibration
Page A4
Rev. 1
GTX 330 Airborne ATC/Mode S Transponder Equipment
010-00230–( ), which includes 011-00455–( )
TSO – C112 Class 2A, and TSO - C74c Class 1A
004-00099-00 Minimum Performance Specification
GARMIN INTERNATIONAL
1200 E 151st St, Olathe, Kansas 66062
RTCA DO-160D
Section
4.0
Equipment tested to Categories A2 B2 F1
4.5.1
-45 degrees C
4.5.2. & 4.5.3
+70 degrees C
4.5.4
Cooling air not required but highly recommended
4.6.1
55,000 Feet
4.6.2
4.6.3
5.0
Equipment tested to Category B
6.0
Equipment tested to Category A
7.0
Equipment tested to Category B
8.0
Equipment tested in each aircraft type to aircraft zone 2.
Aircraft Type 2 and 6 were tested to Category S2,
Vibration level B2. Aircraft Type 3, 4, and 5 were tested
to Category S, Vibration level M.
Note: DO-160D vibration level M modified to increase
level to RTCA DO-160C Curve N for Helicopters as
follows-0.1 inches peak-to-peak double amplitude from
5 Hz to 17 Hz, 1.5g-Pk from 17 Hz to 500 Hz.
Description of Conducted Tests
GTX 330 Installation Manual
190-00207-02